Research on the flame oscillation characteristics of scramjet combustor equipped with strut fuel injector

Author:

Quan Fuxu,Chang JuntaoORCID,Lv Chengkun,Kong Chen,Huang RenzheORCID

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference70 articles.

1. Review of combustion stabilization for hypersonic airbreathing propulsion;Liu;Prog. Aero. Sci.,2020

2. Flame propagation and stabilization in dual-mode scramjet combustors: a survey;Huang;Prog. Aeosp. Sci.,2018

3. Behaviors of the reacting flowfield during the spontaneous formation of ramjet mode under a supersonic inflow;Wang;Phys. Fluids,2023

4. Effects of fuel injection angle on mixing performance of scramjet pylon-cavity flameholder;Oamjee;Phys. Fluids,2020

5. Ignition dynamics and combustion mode transitions in a rocket-based combined cycle combustor operating in the ramjet/scramjet mode;An;Aero. Sci. Technol.,2022

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